Abstract
The problem of gain adjustment in an existing control law is cast into the framework of modern control theory, which results in a real-diagonal block structure of gains to be adjusted. The desire to recover performance in the form of input-output properties, as well as handling qualities, is introduced as a mixed cost functional. LMI-based solutions for H∞and H2based optimization are discussed, as well as a Quasi-Newton approach. The handling qualities of the F/A-18 HARV during refueling serves as a motivating example for the method. Five gains in the existing flight control system are adjusted to recover the performance and handling qualities of the standard F/A-18.
Original language | English (US) |
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Title of host publication | 1997 Guidance, Navigation, and Control Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
Pages | 144-154 |
Number of pages | 11 |
State | Published - Jan 1 1997 |
Externally published | Yes |